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The effect of front-to-rear propeller spacing on the interaction noise at cruise conditions of a model counterrotation propeller having a reduced diameter aft propellerThe effect of forward-to-aft propeller spacing on the interaction noise of a counterrotation propeller with reduced aft diameter was measured at cruise conditions. In general, the tones at 100 percent speed decreased from close to nominal spacing as expected from a wake decay model. However, when the spacing was further increased to the far position, the noise did not decrease as expected and in some cases increased. The behavior at the far spacing was attributed to changing forward propeller performance, which produced larger wakes. The results of this experiment indicate that simple wake decay model is sufficient to describe the behavior of the interaction noise only if the aerodynamic coupling of the two propellers does not change with spacing. If significant coupling occurs such that the loading of the forward propeller is altered, the interaction noise does not necessarily decrease with larger forward-to-aft propeller spacing.
Document ID
19890001232
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dittmar, James H.
(NASA Lewis Research Center Cleveland, OH, United States)
Gordon, Eliott B.
(Sverdrup Technology, Inc., Cleveland Ohio., United States)
Jeracki, Robert J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1988
Subject Category
Acoustics
Report/Patent Number
NAS 1.15:101329
E-4340
NASA-TM-101329
Accession Number
89N10603
Funding Number(s)
PROJECT: RTOP 535-03-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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